Computational design of a high-efficiency accelerator grid for a miniature ion thruster by full-aperture ion optics simulations

Full-aperture ion optics simulations have been conducted for the inhomogeneous plasma source of a miniature ion propulsion system (MIPS) to design a high-efficiency accelerator grid that provides high degree of the neutral confinement and absence of direct ion impingement. The designed accelerator g...

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Main Authors: M. Nakano, K. Nakamura, Y. Naito, Y. Nakagawa, Y. Takao, H. Koizumi
Format: Article
Language:English
Published: AIP Publishing LLC 2019-03-01
Series:AIP Advances
Online Access:http://dx.doi.org/10.1063/1.5090413
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spelling doaj-733d61671fec47f4bf92d1771d2935542020-11-24T21:59:12ZengAIP Publishing LLCAIP Advances2158-32262019-03-0193035343035343-1010.1063/1.5090413086903ADVComputational design of a high-efficiency accelerator grid for a miniature ion thruster by full-aperture ion optics simulationsM. Nakano0K. Nakamura1Y. Naito2Y. Nakagawa3Y. Takao4H. Koizumi5Department of Engineering, Tokyo Metropolitan College of Industrial Technology, 8-17-1, Minami-senjyu, Arakawa-ku, Tokyo 113-0852, JapanDepartment of Systems Integration, Yokohama National University, 79-5 Tokiwadai, Hodogaya, Yokohama 240-8501, JapanDepartment of Advanced Energy, The University of Tokyo, 5-1-5, Kashiwanoha, Kashiwa 277-8561, JapanDepartment of Aeronautics and Astronautics, The University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, JapanDepartment of Systems Integration, Yokohama National University, 79-5 Tokiwadai, Hodogaya, Yokohama 240-8501, JapanDepartment of Advanced Energy, The University of Tokyo, 5-1-5, Kashiwanoha, Kashiwa 277-8561, JapanFull-aperture ion optics simulations have been conducted for the inhomogeneous plasma source of a miniature ion propulsion system (MIPS) to design a high-efficiency accelerator grid that provides high degree of the neutral confinement and absence of direct ion impingement. The designed accelerator grid has flat upstream and smoothly curved downstream surfaces with straight holes for easy low-cost manufacture. The diameter of the accelerator aperture was changed from the nominal value of 0.40 mm to 0.25 mm, which decreased neutral leakage and increased the propellant utilization efficiency from 31 to 50%. The direct impingement of ions caused by decreasing the accelerator aperture diameter was compensated by reducing the thickness of the accelerator grid while taking into account the inhomogeneous ion beam current density profile of the MIPS. An off-design performance simulation was conducted to validate the proposed grid design; the obtained results showed that the ion beam could be accelerated smoothly even during throttling the beam current between 75 and 150%. A grid wear simulation was also performed to compare the changes in the propellant utilization efficiency between the nominal and high-efficiency grids caused by erosion. It was found that the propellant utilization efficiency of the high-efficiency grid was greater than that of the nominal grid within the first 5,000 h of operation and that its lifetime exceeded 10,000 h of the accumulated operation time. By using the proposed high-efficiency accelerator grid and MIPS plasma source, the propellant utilization efficiency was increased, while the accelerator impingement current became negligible.http://dx.doi.org/10.1063/1.5090413
collection DOAJ
language English
format Article
sources DOAJ
author M. Nakano
K. Nakamura
Y. Naito
Y. Nakagawa
Y. Takao
H. Koizumi
spellingShingle M. Nakano
K. Nakamura
Y. Naito
Y. Nakagawa
Y. Takao
H. Koizumi
Computational design of a high-efficiency accelerator grid for a miniature ion thruster by full-aperture ion optics simulations
AIP Advances
author_facet M. Nakano
K. Nakamura
Y. Naito
Y. Nakagawa
Y. Takao
H. Koizumi
author_sort M. Nakano
title Computational design of a high-efficiency accelerator grid for a miniature ion thruster by full-aperture ion optics simulations
title_short Computational design of a high-efficiency accelerator grid for a miniature ion thruster by full-aperture ion optics simulations
title_full Computational design of a high-efficiency accelerator grid for a miniature ion thruster by full-aperture ion optics simulations
title_fullStr Computational design of a high-efficiency accelerator grid for a miniature ion thruster by full-aperture ion optics simulations
title_full_unstemmed Computational design of a high-efficiency accelerator grid for a miniature ion thruster by full-aperture ion optics simulations
title_sort computational design of a high-efficiency accelerator grid for a miniature ion thruster by full-aperture ion optics simulations
publisher AIP Publishing LLC
series AIP Advances
issn 2158-3226
publishDate 2019-03-01
description Full-aperture ion optics simulations have been conducted for the inhomogeneous plasma source of a miniature ion propulsion system (MIPS) to design a high-efficiency accelerator grid that provides high degree of the neutral confinement and absence of direct ion impingement. The designed accelerator grid has flat upstream and smoothly curved downstream surfaces with straight holes for easy low-cost manufacture. The diameter of the accelerator aperture was changed from the nominal value of 0.40 mm to 0.25 mm, which decreased neutral leakage and increased the propellant utilization efficiency from 31 to 50%. The direct impingement of ions caused by decreasing the accelerator aperture diameter was compensated by reducing the thickness of the accelerator grid while taking into account the inhomogeneous ion beam current density profile of the MIPS. An off-design performance simulation was conducted to validate the proposed grid design; the obtained results showed that the ion beam could be accelerated smoothly even during throttling the beam current between 75 and 150%. A grid wear simulation was also performed to compare the changes in the propellant utilization efficiency between the nominal and high-efficiency grids caused by erosion. It was found that the propellant utilization efficiency of the high-efficiency grid was greater than that of the nominal grid within the first 5,000 h of operation and that its lifetime exceeded 10,000 h of the accumulated operation time. By using the proposed high-efficiency accelerator grid and MIPS plasma source, the propellant utilization efficiency was increased, while the accelerator impingement current became negligible.
url http://dx.doi.org/10.1063/1.5090413
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